AD 2013-24035

final rule
Data completeness: 70%

Airworthiness Directives; Bell Helicopter Textron Canada Limited (Bell) Helicopters

AD Number
2013-24035
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2013-0491
FR Citation
78 FR 65206

Applicability

TypeManufacturerModelDetails
aircraft Textron Various Airworthiness Directives; Bell Helicopter Textron Canada Limited (Bell) Helicopters
aircraft Bell 430 Airworthiness Directives; Bell Helicopter Textron Canada Limited (Bell) Helicopters

Unsafe Condition

Third stage turbine vibration, which could result in turbine failure, engine power loss, and subsequent loss of control of the helicopter.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Revise the Operating Limitations section of the Model 430 Rotorcraft Flight Manual by inserting Section 1, Limitations, page 1-7, of Bell BHT-430-FM-1, revision 18, dated September 1, 2009. Install placard part number 230-075-213-113-113, or equivalent, on the instrument panel directly below the pilot audio select panel.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 30 days

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Bell Model 430 helicopters, serial number 49001 through 49111, certificated in any category.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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